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Instrument error analysis as it applies to wind-tunnel testingErrors resulting from the instrumentation used to measure wind tunnel model parameters are analyzed. The pertinent parameters, their standard deviations, and the theoretical derivation of them, are given. Some BASIC programs and plots for the standard deviations of dynamic pressure, Mach number, and Reynolds number are included.
Document ID
19800005175
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Rind, E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1979
Subject Category
Instrumentation And Photography
Report/Patent Number
L-13222
NASA-TP-1572
Report Number: L-13222
Report Number: NASA-TP-1572
Accession Number
80N13430
Funding Number(s)
PROJECT: RTOP 505-31-63-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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